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Brush Seals for Improved Steam Turbine PerformanceGE Energy has retrofitted brush seals into more than 19 operating steam turbines. Brush seals offer superior leakage control compared to labyrinth seals, owing to their compliant nature and ability to maintain very tight clearances to the rotating shaft. Seal designs have been established for steam turbines ranging in size from 12 MW to over 1200 MW, including fossil, nuclear, combined-cycle and industrial applications.

Steam turbines present unique design challenges that must be addressed to ensure that the potential performance benefits of brush seals are realized. Brush seals can have important effects on the overall turbine system that must be taken into account to assure reliable operation. Subscale rig tests are instrumental to understanding seal behavior under simulated steam-turbine operating conditions, prior to installing brush seals in the field. This presentation discusses the technical challenges of designing brush seals for steam turbines; subscale testing; performance benefits of brush seals; overall system effects; and field applications
Document ID
20070002978
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Norman Turnquist
(GE Global Research (United States) Niskayuna, United States)
Ray Chupp
(GE Global Research (United States) Niskayuna, United States)
Fred Baily
(General Electric (United States) Boston, United States)
Mark Burnett
(General Electric (United States) Boston, United States)
Flor Rivas
(General Electric (United States) Boston, United States)
Aaron Bowsher
(Cross Manufacturing Company Bath, United Kingdom)
Peter Crudgington
(Cross Manufacturing Company Bath, United Kingdom)
Date Acquired
August 24, 2013
Publication Date
October 1, 2006
Publication Information
Publication: 2005 NASA Seal/Secondary Air System Workshop
Publisher: National Aeronautics and Space Administration
Volume: 1
Subject Category
Space Transportation And Safety
Report/Patent Number
NASA/CP-2006-214383/VOL1
Meeting Information
Meeting: NASA Seal/Secondary Air System Workshop
Location: Cleveland, OH
Country: US
Start Date: November 8, 2005
End Date: November 9, 2005
Sponsors: National Aeronautics and Space Administration
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
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